Pilatus PC-7

The Pilatus PC-7 Turbo Trainer is a low-wing tandem-seat training aircraft, designed and manufactured in Switzerland by Pilatus Aircraft. The aircraft is capable of all basic training functions, including aerobatics, instrument, tactical, and night flying. The PC-7 was developed from the preceding piston-powered Pilatus P-3, largely differing by the adoption of a turboprop engine, a bubble canopy, and a new one-piece wing. It is powered by a Pratt & Whitney Canada PT6A-25A turboprop engine rated at 410 kilowatts (550 shaft horsepower), driving a three-bladed Hartzell constant-speed propeller.

The PC-7 has a crew of two, a length of 9.78 m, wingspan of 10.40 m, and a max takeoff weight of 2,700 kg. Its maximum speed is 412 km/h (222 knots), service ceiling is 10,060 m (33,000 ft), and standard range is 1,200 km, with a ferry range of 2,630 km. The PC-7 is an entry-level turboprop trainer renowned for its simplicity, durability, and reduced operating cost. It has developed a sizable presence of the global trainer market and has been adopted by twenty air forces as their ab initio trainer, as well as multiple civilian operators. More than 600 PC-7 family airframes have been produced, and its forgiving handling and reliable airframe make it suited for primary flight training.

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What is the Pilatus PC-7 aircraft?

The Pilatus PC-7 aircraft is a two-seat basic trainer aircraft, powered by a PT6A-25A engine rated at 410 kilowatts (550 shaft horsepower). This aircraft is an entry-level turboprop trainer, renowned for its simplicity, durability, and reduced operating cost. The Pilatus PC-7 Turbo Trainer is a low-wing, tandem-seat training aircraft manufactured by Pilatus Aircraft. It is capable of all basic training functions, including aerobatics instrument tactical and night flying. The PC-7 MKX is the only trainer aircraft in this class equipped with the Martin-Baker ejection seats and Pratt & Whitney Canada engine.

The two cockpits, arranged one behind the other, are equipped with flight and navigation instruments that allow advanced instrument flight training. The PC-7 MKX is equipped with state-of-the-art avionics software. It has a glass cockpit with PFD, EFIS glass, and MFD. It also has a HUD, HighwayInTheSky, and a computer-made picture of what is in front. A traffic warning system and a cockpit camera with touch panel are included. Early PC-7 aircraft have a panel with analog cockpit gauges.

The PC-7 has six hardpoints. These add rapid fire guns, dummy bombs (using bomb tubes), and missiles. The PC-7s were typically deployed armed with a mixture of gun pods and rocket pods. But the sale of combat-capable aircraft has been controversial. Political pressure has been applied for PC-7s to be shipped without the fittings for armaments being installed.

The PC-7 is used by the Swiss Air Force for basic training, selection of new military pilots, the PC-7 TEAM demonstrations, and liaison flights. It has been used in more than 20 countries as an entry platform for military pilot training. It has been adopted by twenty air forces as their ab initio trainer, as well as multiple civilian operators. A kit of new avionics for the type, which included a new mission computer, a wide-angle head-up display, and replacement communications and weapons-delivery systems, was offered. So, the trainer communications were modernized.

The PC-7 MKX is the only trainer in this class equipped with Martin-Baker ejection seats. It has fuel tanks beneath the wings with a typical capacity of 474 L (125 US gal) and extra fuel pods of 240 L (63 US gal). It can take off in 285 meters (935 feet). The airframe has a durability of 2,500 hours in the sky and can stop ten thousand times in the air. Over 600 PC-7s have been built, and about 385 are in active service in 2026 across 18 nations. Air forces like India (75 PC-7 Mark II ordered, 35 delivered), France (22), Belgium (18), and the Netherlands (8) operate it.

What is the Pilatus PC-7 Mk II?

The Pilatus PC-7 Mk II is a trainer aircraft manufactured by Pilatus Aircraft. It is powered by a PT6A-25C engine of 522 kilowatts (700 shaft horsepower), rather than the PT6A-62 of the PC-9. It retains the PC-7's wing while using a refined version of the PC-9's airframe. It first flew on 28 September 1992, and it was introduced in 1994. It can mount external stores.

The Pilatus PC-7 Mk II is an upgraded model developed during the 1990s. It combines the newer airframe and avionics from the PC-9 with the PC-7's smaller turbine engine. TDeveloped for the South African Air Force, it is known as the 'Astra'. The SAAF was the first customer and ordered 60 units in 1993. The aircraft has a four blade propeller and a South African developed avionics suite. The Indian Air Force currently operates 75 PC-7 Mk II aircraft for basic training. The Indian Coast Guard also uses the PC-7 Mk II.

Powered by a PT6A-25C of 522 kilowatts (700 shaft horsepower), the engine is not as robust as the PC-9's PT6A-62. The PC-7 Mk II has tandem seating with ejection seats, and the cockpit is not under pressure. Maximum weight in everyday setup is about 2.8 tonnes, and in stunt setup a little over 2.5 tons. Fuel tankage is 500 liters (133 American gallons), and it can have underwing gas containers. Each underwing container has about 53 gallons (200.6 liters), so with them total capacity is about 904 quarts (855.5 liters) or 238.8 American gallons (904 liters). Stall speed is 75 knots (86.3 miles per hour), or 77 knots calibrated airspeed (88.6 miles per hour), and endurance is +7g (68.6 meters per second squared) and -3.5g (34.3 meters per second squared). The unit cost is about 38.5 crore rupees, or $4.6 million. The PC-7 Mk II’s production count is 250, but the PC-7 group has 5 versions and aggregate production of more than 500, with total planes made hitting 628. Originally the PC-7 Mk II had an analog cockpit, but later it was upgraded but it did not have advanced instrumentation.

What are the specifications of the Pilatus PC-7?

The specifications of the Pilatus PC-7 are given in the table below.

The Pilatus PC-7 has a crew of two, a student pilot and a pilot instructor. Max landing weight is 5,655 lb (2,565 kg), and max zero fuel weight is 4,409 lb (2,000 kg). The powerplant is one Pratt & Whitney Canada PT6A-25A turboprop, 410 kW. Maximum speed is 256 mph (412 km/h) at 20,000 ft (6,095 m), and cruise speed is 196 mph (316 km/h). The aircraft has a top speed of 256 mph (412 km/h). Stall speed is 74 mph (119 km/h) with flaps and gear down. Rate of climb is 10.9 m/s (35.8 ft/s), and climb to 5,000 m (16,404 ft) takes 9 min 0 sec (0.15 hr). Due to the PT6A-25A engine, the PC-7 has a service ceiling of 33,005 ft (10,060 m). G limits are +6 and -3. Take-off run is 780 m (2,559 ft) at max take-off weight, and landing run is 505 m (1,657 ft) at max landing weight. Range is 745.65 miles (1,200 km) without external drop tanks, and ferry range is 1,634.16 miles (2,630 km). Endurance is 4 hr 22 min.

What is the performance of the Pilatus PC-7?

The performance of the Pilatus PC-7 is given in the table below.

The Pilatus PC-7 Turbo Trainer has a top speed of 412 km/h (256 mph). The PC-7 MKX has a top speed of 300 knots. Cruise speed is 196 mph (316 km/h) economy cruise, and normal cruise speed is 411 km/h (222 knots). The standard range is 1,200 km (746 miles), and ferry range with external drop tanks is 2,630 km (1,634 miles).

What is the price of the Pilatus PC-7?

The price of the Pilatus PC-7 varies by year, configuration, and demilitarisation status. For used aircraft, public listings in 2024-2025 showed asking prices from about $595,000 for late-1970s airframes to around $900,000 for newer, low-time examples. A demilitarised civilian PC-7’s price range is $750,000 to $1,000,000. An atypical price point is $1,400,000, like a PC-7 Turbo Trainer. Price relies on lifespan, hours run since condition, overhaul, and electronics setup. Modern dashboard improvements raise price by 5 to 10 out of every 100, and a Garmin G950 plane electronics gear adds a premium of $300,000 to $500,000. Original factory guarantee on modifications keeps resale value, but modifications without official approval lower price by 10 to 15 out of every 100. Ejection seats add $80,000 to $120,000 and better propellers add $40,000 to $70,000. Engine overhaul adds about 15 percent.

The Pilatus PC-7 Mk II does not have a checked asking price. The Indian Air Force deal for 75 Pilatus PC7 MkII aircraft is $523 million, which is $6.97 million per aircraft, and has spares, training, and ground tools. A deal for 22 PC-7 MKX planes has a value of about EUR 795 million, or about USD 37 million per aircraft, with learning tools, support, and fixing plans. Pilatus believed newly built examples would be priced between $1 million and $2 million. However, standard base price estimates are $3.5 to $4.5 million, with integration packages between $5 and $6 million. Pilatus’ starting price is $4.4 million per unit. Expenses for turboprops average $1,200 to $1,800 per hour in the air. Engine reserves are $250 to $450 per hour. Small plane deep checks cost $300,000 to $700,000 every 8 to 12 years. Effective price perception goes down by 10 to 20 out of every 100 within 1.5 years of a heavy maintenance.